JP3106206U - A device that blocks birds from entering the jet engine and removes birds from the intake area - Google Patents
A device that blocks birds from entering the jet engine and removes birds from the intake area Download PDFInfo
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- JP3106206U JP3106206U JP2004003569U JP2004003569U JP3106206U JP 3106206 U JP3106206 U JP 3106206U JP 2004003569 U JP2004003569 U JP 2004003569U JP 2004003569 U JP2004003569 U JP 2004003569U JP 3106206 U JP3106206 U JP 3106206U
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Abstract
【課題】鳥のエンジンへの衝突後にも充分な吸気の確保を図る為に、鳥を吸気口でブロックするだけではなく、吸気エリアからの鳥の排除ができる装置を提供する。
【解決手段】通気口を設けた半球形の金属製のカバー1をエンジンの吸気口前に設置し、鳥のエンジンへの衝突をブロックすると共に、カバーを高速で回転させる事により鳥をカバーより排除するものです。エンジンの吸気ファンの回転11を減速歯車群5を介してカバーの回転軸に伝え、カバーの高速回転による強い遠心力と強い気流により、衝突した鳥をカバー外へと飛ばすものです。
【選択図】図1An object of the present invention is to provide a device that not only blocks birds at an intake port but also eliminates birds from an intake area in order to ensure sufficient intake even after a bird collides with an engine.
A hemispherical metal cover provided with a vent is installed in front of an intake port of an engine to block birds from colliding with the engine and to rotate the cover at a high speed so that birds can be removed from the cover. To eliminate. The rotation 11 of the intake fan of the engine is transmitted to the rotation axis of the cover via the reduction gear group 5, and the high-speed rotation of the cover causes strong centrifugal force and strong airflow to fly the colliding bird out of the cover.
[Selection diagram] Fig. 1
Description
本装置は、ジェット機の飛行中における鳥のエンジンへの吸い込みを防止、鳥をエンジン吸気口より排除する装置に関するものです。This device relates to a device that prevents birds from being sucked into the engine during the flight of a jet aircraft and removes birds from the engine intake.
現在、ジェット機は、空気をエンジン吸気口を通して直接吸気ファンにより吸気している為、鳥がエンジンの軌道エリアに進入した場合は、鳥の吸気ファンや燃焼室等への衝突が想定されます。エンジンの保護の為エンジン吸気口の前に網状のカバーを設置した場合、鳥の衝突による吸気面積の大幅な縮小を来たします。また強い吸気圧力により鳥の排除にも結びつかない事より、ジェット機のバード・ストライク対策は主に吸気ファンの強度向上をメインに推進されて来ております。At present, jet aircraft draws air directly through the engine intake port by the intake fan, so if a bird enters the orbital area of the engine, it is expected that the bird will collide with the intake fan or combustion chamber. If a net-shaped cover is installed in front of the engine intake to protect the engine, the intake area will be significantly reduced due to bird collision. In addition, birds are not eliminated due to strong intake pressure, and bird strike measures for jet aircraft are mainly promoted by improving the strength of intake fans.
近年、ジェット機の普及、空港の増加を受け、鳥のエンジン吸気口からの進入による事故、トラブルのリスクが増大しています。現在普及しているジェット機の主流は、エンジン前部に吸気ファンを設置し機体前方の空気を高圧で吸気・圧縮し、燃焼機関へ送り込み、高速飛行を実現しています。鳥が飛行機のエンジン部の飛行軌道に進入すると、吸気ファン、気流によりエンジンへ吸い込まれます。 このような事故が起こった場合、吸気ファンやコンプレッサーの破損等、エンジンへのダメージも大きく、多額の修理費は元より、墜落等、搭乗者の生命を危険にさらす事態が想定されます。この問題を抜本的に解決し、鳥衝突後にも充分な吸気の確保を図る為には、鳥を吸気口でブロックすると共に、吸気エリアからの鳥の排除が不可欠です。In recent years, with the spread of jet aircraft and the increase in airports, the risk of accidents and troubles due to birds entering through the engine intake has increased. The mainstream jet aircraft currently in use installs an intake fan at the front of the engine, inhales and compresses the air in front of the aircraft at high pressure, sends it to the combustion engine, and achieves high-speed flight. When the bird enters the flight trajectory of the engine part of the airplane, it is sucked into the engine by the intake fan and airflow. If such an accident occurs, damage to the engine, such as damage to the intake fan or compressor, will be large, and large amounts of repair costs, as well as crashes, may endanger the occupants' lives. In order to drastically solve this problem and ensure sufficient intake even after a bird collision, it is essential to block birds at the intake and remove birds from the intake area.
本考案は、この鳥問題解決の為、回転軸を中心に回転する多数の通気口を設けた半球形の金属製のカバーをジェット機の全てのエンジンの吸気口前部に取り付けるものです。図1の様にカバー外壁板はフレームを介して回転軸に固定されており、カバーの回転軸はエンジンの吸気ファンの回転軸に減速歯車群を介して取り付けられており、カバーは回転軸を中心に回転する仕組みになっています。In order to solve this bird problem, the present invention attaches a hemispherical metal cover provided with a number of vents that rotate around the rotation axis to the front of the intake port of all engines of the jet. As shown in FIG. 1, the cover outer wall plate is fixed to a rotating shaft via a frame, the rotating shaft of the cover is attached to a rotating shaft of an intake fan of the engine via a group of reduction gears, and the cover is connected to the rotating shaft. It is designed to rotate around the center.
カバーの回転軸に設置されている圧力センサーが、カバーへの鳥の衝突を検出すると、即座に電磁石を使ったアクチュエーターによりエンジンの吸気ファンの回転がカバーの回転軸に伝えられます。するとカバーが高速回転し、強い遠心力と機体後方への強い気流により、鳥がカバー外へ飛ばされます。これにより吸気エリアからの鳥の排除、鳥衝突後も充分な吸気の確保、安全なフライトが実現できます。When a bird's collision with the cover is detected by a pressure sensor installed on the rotating shaft of the cover, the rotation of the engine's intake fan is immediately transmitted to the rotating shaft of the cover by an actuator using electromagnets. Then, the cover rotates at a high speed, and the bird is blown out of the cover by the strong centrifugal force and the strong airflow behind the aircraft. This eliminates birds from the intake area, ensures sufficient intake even after a bird collision, and realizes a safe flight.
下記の仕様・設計により従来の吸気効率を維持しつつ、鳥問題のリスクの低減を図ります。多数の通気口を設けた半球形のカバーの採用により、大きなロス無しにエンジンの吸気の確保を図ることが可能です。 カバーの外壁板は、四分割されたブロック毎に、打ち抜き成型により製造され、リベット等により組み立てられ、フレームを介して回転軸に固定されています。The following specifications and designs maintain the conventional intake efficiency and reduce the risk of bird problems. The use of a hemispherical cover with numerous vents makes it possible to secure the intake of the engine without significant loss. The outer wall plate of the cover is manufactured by stamping, for each block divided into four, assembled with rivets, etc., and fixed to the rotating shaft via a frame.
多数の通気口を設けた半球形のカバーの採用により、エンジン吸気口への鳥の進入をブロックする事が可能。 平板状の円形の格子をジェットエンジン吸気口に設置した場合と比較して、半球形のカバーの場合はより大きい吸気面積(約2倍)が確保できる為、鳥が一羽衝突、吸気面積の減少を来たしても、その他の面積からの吸気の確保が可能となります。The adoption of a hemispherical cover with a number of vents makes it possible to block birds from entering the engine intake. Compared to the case where a flat circular grid is installed at the jet engine inlet, the hemispherical cover can secure a larger intake area (about twice), so that one bird collides and the intake area becomes smaller. Even if it decreases, it is possible to secure intake from other areas.
鳥衝突時に、吸気ファンの回転をカバーの回転につなげることにより、カバーの回転運動による遠心力で鳥をカバー外へ跳ね飛ばし、吸気の確保を図る。ここでは、吸気ファンの高速回転を利用し、減速歯車群を介してカバーの回転に結び付けています。At the time of a bird collision, the rotation of the intake fan is linked to the rotation of the cover, so that the birds fly out of the cover by centrifugal force due to the rotational movement of the cover to secure the air intake. Here, using the high-speed rotation of the intake fan, it is linked to the rotation of the cover via a group of reduction gears.
カバーとエンジン回転軸の接合部に、エンジン前方からのカバーへの圧力を感知するセンサーを組み込むことにより、圧力変化の波形パターン分析により鳥の衝突を感知し、高速なファンの回転軸の回転を電磁石式のアクチュエーターにより即座にカバーの回転に伝える。 この遠心力と気流により鳥をカバー外へ跳ね飛ばし、吸気エリアの確保を図る。By incorporating a sensor that senses pressure from the front of the engine to the cover at the joint between the cover and the engine rotation axis, birds' collision is detected by analyzing the waveform pattern of the pressure change, and high-speed rotation of the rotation axis of the fan is achieved. Immediately transmit the rotation of the cover by an electromagnetic actuator. By this centrifugal force and airflow, birds are bounced out of the cover to secure an intake area.
カバーの先端部よりエンジン後方にかけて回転軸から外周までの半径がより大きくなる様に、半球形の形状を採用していることにより、一番空気抵抗の大きい先端部に衝突した鳥は遠心力と強い風圧により、半球形の後方部へ押しやられる。 半球形の後方部分ではより強い遠心力と風圧により、鳥をカバーの外へと跳ね飛ばします。By adopting a hemispherical shape so that the radius from the rotating shaft to the outer circumference becomes larger from the tip of the cover to the rear of the engine, the bird that collides with the tip with the largest air resistance will have centrifugal force and The strong wind pressure pushes it towards the hemispherical rear. In the rear part of the hemisphere, the birds bounce out of the cover due to the stronger centrifugal force and wind pressure.
鳥が衝突していない時は、アクチュエーターが動作していない為、エンジンの吸気ファンの回転はカバーの回転には伝達されない為、エンジンへの負荷・負担は抑えられます。軽く、硬質な金属板の採用によりカバーの軽量化を図り、エンジンへの構造的な負担の軽減を図ります。When the bird does not collide, the rotation of the engine intake fan is not transmitted to the rotation of the cover because the actuator is not operating, so the load and load on the engine is reduced. The adoption of a light and hard metal plate reduces the weight of the cover and reduces the structural burden on the engine.
カバーの高速回転によりカバー先端部より螺旋状の気流が発生、これと遠心力、機体後方への気流を利用し、鳥をカバー外へと飛ばします。The high-speed rotation of the cover generates a spiral airflow from the tip of the cover, and uses this, centrifugal force, and airflow to the rear of the aircraft to fly the bird out of the cover.
鳥がカバーに衝突し、小さな骨片に飛散した場合を想定し、更に目の細かい格子で出来た細かい格子状の板を図1の様に設置することによりダブルブロックを図る事も可能です。Assuming that a bird collides with the cover and scatters on a small bone fragment, it is possible to create a double block by installing a fine grid-like plate made of a finer grid as shown in Fig. 1.
アクチュエーターには、電磁石を採用する事により、エンジン回転軸の回転数の多段階でのカバー軸への伝達率のコントロールが可能です。 鳥が衝突したエンジンと他のエンジンの出力バランスを考慮し、当該カバーへの伝達率を制御する事も可能です。By using an electromagnet for the actuator, it is possible to control the transmission rate to the cover shaft in multiple stages of the rotation speed of the engine rotation shaft. It is also possible to control the transmission rate to the cover in consideration of the output balance of the engine that the bird collided with the other engine.
図1にて実施例を示します。
センサーを使用せず、常時カバーを吸気ファンの回転軸に接続させて、常時カバーを回転させておくことも可能です。 空港周辺での離着陸時は元より、フライト中も常時カバーを回転させておくことも可能です。また、高度計とコンピュータとの接続により、バードストライク(鳥のエンジンからの吸気問題)のリスクの高い離着陸時の高度になった場合に自動的ににカバーを回転させる事も可能です。Fig. 1 shows an embodiment.
It is also possible to keep the cover rotating at all times by connecting the cover to the rotation axis of the intake fan without using a sensor. The cover can be rotated at all times during the flight as well as during takeoff and landing near the airport. In addition, by connecting the altimeter to the computer, it is possible to automatically rotate the cover when the altitude at the time of takeoff and landing with a high risk of bird strike (problem of intake from the bird engine).
1 カバー外壁版
2 フレーム
3 カバー回転軸
4 先端部
5 減速歯車群
6 細かい格子状の板
7 エンジン前部
8 フレーム
9 吸気ファン
10 低圧コンプレッサー
11 吸気ファン回転軸DESCRIPTION OF SYMBOLS 1 Cover outer wall slab 2 Frame 3 Cover rotating shaft 4 Tip 5 Reduction gear group 6 Fine grid-like plate 7 Engine front 8 Frame 9 Intake fan 10 Low pressure compressor 11 Intake fan rotation shaft
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JP2004003569U JP3106206U (en) | 2004-05-24 | 2004-05-24 | A device that blocks birds from entering the jet engine and removes birds from the intake area |
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JP2004003569U JP3106206U (en) | 2004-05-24 | 2004-05-24 | A device that blocks birds from entering the jet engine and removes birds from the intake area |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0658688A (en) * | 1992-08-11 | 1994-03-04 | Mitsubishi Shindoh Co Ltd | Inner surface grooved weld copper alloy pipe |
WO2011099383A1 (en) * | 2010-02-10 | 2011-08-18 | 有限会社 奥戸溶接 | Aircraft |
JP2015117688A (en) * | 2013-12-18 | 2015-06-25 | 有▲吉▼ 一夫 | Bird strike arrestor enabling safe flight even if jet engine sucks obstacles such as birds, pebbles and ice pieces and the like |
JP2015218722A (en) * | 2014-05-21 | 2015-12-07 | 一夫 有▲吉▼ | Bird strike prevention device enabling safe flying to be carried out even if foreign materials such as birds, small stones and ice pieces or the like are sucked |
JP2019156380A (en) * | 2018-03-11 | 2019-09-19 | 妹尾 淑子 | Vertical takeoff and landing flight vehicle with foreign matter removal movable part |
JP7430460B2 (en) | 2020-09-29 | 2024-02-13 | 三菱マヒンドラ農機株式会社 | work vehicle |
-
2004
- 2004-05-24 JP JP2004003569U patent/JP3106206U/en not_active Expired - Fee Related
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0658688A (en) * | 1992-08-11 | 1994-03-04 | Mitsubishi Shindoh Co Ltd | Inner surface grooved weld copper alloy pipe |
WO2011099383A1 (en) * | 2010-02-10 | 2011-08-18 | 有限会社 奥戸溶接 | Aircraft |
JP2015117688A (en) * | 2013-12-18 | 2015-06-25 | 有▲吉▼ 一夫 | Bird strike arrestor enabling safe flight even if jet engine sucks obstacles such as birds, pebbles and ice pieces and the like |
JP2015218722A (en) * | 2014-05-21 | 2015-12-07 | 一夫 有▲吉▼ | Bird strike prevention device enabling safe flying to be carried out even if foreign materials such as birds, small stones and ice pieces or the like are sucked |
JP2019156380A (en) * | 2018-03-11 | 2019-09-19 | 妹尾 淑子 | Vertical takeoff and landing flight vehicle with foreign matter removal movable part |
JP7430460B2 (en) | 2020-09-29 | 2024-02-13 | 三菱マヒンドラ農機株式会社 | work vehicle |
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